Self-sensing surface radar structure for hypersonic flight environment

Self-sensing surface radar structure for hypersonic flight environment

The invention belongs to the technical field of surface radars, and particularly relates to a self-sensing surface radar structure for a hypersonic flight environment. A phase change/air cooling passive thermal insulation layer, a radiation array surface layer and a power division network layer all...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: WANG WEI, LI PENG, XU WANYE, LIU JUAN, WANG QUNBIAO, FAN ZIJIAO, LI NA, ZHANG CHAO, SONG LIWEI, CHEN BO
Format: Patent
Sprache:chi ; eng
Schlagworte:
ANTENNAS, i.e. RADIO AERIALS
BASIC ELECTRIC ELEMENTS
ELECTRICITY
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator WANG WEI
LI PENG
XU WANYE
LIU JUAN
WANG QUNBIAO
FAN ZIJIAO
LI NA
ZHANG CHAO
SONG LIWEI
CHEN BO
description The invention belongs to the technical field of surface radars, and particularly relates to a self-sensing surface radar structure for a hypersonic flight environment. A phase change/air cooling passive thermal insulation layer, a radiation array surface layer and a power division network layer all comprise antenna structures, each antenna structure comprises an antenna housing and a conformal array antenna, and each conformal array antenna comprises a conformal feed network, a first dielectric substrate, a grounding plate, a first metal frame, a second dielectric substrate, a second metal frame and a third dielectric substrate which are arranged in sequence. The second dielectric substrate is provided with an arched microstrip double-patch array, and the third dielectric substrate is provided with a conformal parasitic patch array; and aerogel is arranged between the first metal frame and the second dielectric substrate, between the second metal frame and the third dielectric substrate, and between the third
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN117410705A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN117410705A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN117410705A3</originalsourceid><addsrcrecordid>eNrjZHALTs1J0y1OzSvOzEtXKC4tSktMTlUoSkxJLFIoLikqTS4pLUpVSMsvUsioLEgtKs7Py0xWSMvJTM8oUUjNK8ssys_LTc0r4WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFQEPzUkvinf0MDc1NDA3MDUwdjYlRAwCENzRR</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Self-sensing surface radar structure for hypersonic flight environment</title><source>esp@cenet</source><creator>WANG WEI ; LI PENG ; XU WANYE ; LIU JUAN ; WANG QUNBIAO ; FAN ZIJIAO ; LI NA ; ZHANG CHAO ; SONG LIWEI ; CHEN BO</creator><creatorcontrib>WANG WEI ; LI PENG ; XU WANYE ; LIU JUAN ; WANG QUNBIAO ; FAN ZIJIAO ; LI NA ; ZHANG CHAO ; SONG LIWEI ; CHEN BO</creatorcontrib><description>The invention belongs to the technical field of surface radars, and particularly relates to a self-sensing surface radar structure for a hypersonic flight environment. A phase change/air cooling passive thermal insulation layer, a radiation array surface layer and a power division network layer all comprise antenna structures, each antenna structure comprises an antenna housing and a conformal array antenna, and each conformal array antenna comprises a conformal feed network, a first dielectric substrate, a grounding plate, a first metal frame, a second dielectric substrate, a second metal frame and a third dielectric substrate which are arranged in sequence. The second dielectric substrate is provided with an arched microstrip double-patch array, and the third dielectric substrate is provided with a conformal parasitic patch array; and aerogel is arranged between the first metal frame and the second dielectric substrate, between the second metal frame and the third dielectric substrate, and between the third</description><language>chi ; eng</language><subject>ANTENNAS, i.e. RADIO AERIALS ; BASIC ELECTRIC ELEMENTS ; ELECTRICITY</subject><creationdate>2024</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240116&amp;DB=EPODOC&amp;CC=CN&amp;NR=117410705A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240116&amp;DB=EPODOC&amp;CC=CN&amp;NR=117410705A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WANG WEI</creatorcontrib><creatorcontrib>LI PENG</creatorcontrib><creatorcontrib>XU WANYE</creatorcontrib><creatorcontrib>LIU JUAN</creatorcontrib><creatorcontrib>WANG QUNBIAO</creatorcontrib><creatorcontrib>FAN ZIJIAO</creatorcontrib><creatorcontrib>LI NA</creatorcontrib><creatorcontrib>ZHANG CHAO</creatorcontrib><creatorcontrib>SONG LIWEI</creatorcontrib><creatorcontrib>CHEN BO</creatorcontrib><title>Self-sensing surface radar structure for hypersonic flight environment</title><description>The invention belongs to the technical field of surface radars, and particularly relates to a self-sensing surface radar structure for a hypersonic flight environment. A phase change/air cooling passive thermal insulation layer, a radiation array surface layer and a power division network layer all comprise antenna structures, each antenna structure comprises an antenna housing and a conformal array antenna, and each conformal array antenna comprises a conformal feed network, a first dielectric substrate, a grounding plate, a first metal frame, a second dielectric substrate, a second metal frame and a third dielectric substrate which are arranged in sequence. The second dielectric substrate is provided with an arched microstrip double-patch array, and the third dielectric substrate is provided with a conformal parasitic patch array; and aerogel is arranged between the first metal frame and the second dielectric substrate, between the second metal frame and the third dielectric substrate, and between the third</description><subject>ANTENNAS, i.e. RADIO AERIALS</subject><subject>BASIC ELECTRIC ELEMENTS</subject><subject>ELECTRICITY</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHALTs1J0y1OzSvOzEtXKC4tSktMTlUoSkxJLFIoLikqTS4pLUpVSMsvUsioLEgtKs7Py0xWSMvJTM8oUUjNK8ssys_LTc0r4WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFQEPzUkvinf0MDc1NDA3MDUwdjYlRAwCENzRR</recordid><startdate>20240116</startdate><enddate>20240116</enddate><creator>WANG WEI</creator><creator>LI PENG</creator><creator>XU WANYE</creator><creator>LIU JUAN</creator><creator>WANG QUNBIAO</creator><creator>FAN ZIJIAO</creator><creator>LI NA</creator><creator>ZHANG CHAO</creator><creator>SONG LIWEI</creator><creator>CHEN BO</creator><scope>EVB</scope></search><sort><creationdate>20240116</creationdate><title>Self-sensing surface radar structure for hypersonic flight environment</title><author>WANG WEI ; LI PENG ; XU WANYE ; LIU JUAN ; WANG QUNBIAO ; FAN ZIJIAO ; LI NA ; ZHANG CHAO ; SONG LIWEI ; CHEN BO</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN117410705A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>ANTENNAS, i.e. RADIO AERIALS</topic><topic>BASIC ELECTRIC ELEMENTS</topic><topic>ELECTRICITY</topic><toplevel>online_resources</toplevel><creatorcontrib>WANG WEI</creatorcontrib><creatorcontrib>LI PENG</creatorcontrib><creatorcontrib>XU WANYE</creatorcontrib><creatorcontrib>LIU JUAN</creatorcontrib><creatorcontrib>WANG QUNBIAO</creatorcontrib><creatorcontrib>FAN ZIJIAO</creatorcontrib><creatorcontrib>LI NA</creatorcontrib><creatorcontrib>ZHANG CHAO</creatorcontrib><creatorcontrib>SONG LIWEI</creatorcontrib><creatorcontrib>CHEN BO</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WANG WEI</au><au>LI PENG</au><au>XU WANYE</au><au>LIU JUAN</au><au>WANG QUNBIAO</au><au>FAN ZIJIAO</au><au>LI NA</au><au>ZHANG CHAO</au><au>SONG LIWEI</au><au>CHEN BO</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Self-sensing surface radar structure for hypersonic flight environment</title><date>2024-01-16</date><risdate>2024</risdate><abstract>The invention belongs to the technical field of surface radars, and particularly relates to a self-sensing surface radar structure for a hypersonic flight environment. A phase change/air cooling passive thermal insulation layer, a radiation array surface layer and a power division network layer all comprise antenna structures, each antenna structure comprises an antenna housing and a conformal array antenna, and each conformal array antenna comprises a conformal feed network, a first dielectric substrate, a grounding plate, a first metal frame, a second dielectric substrate, a second metal frame and a third dielectric substrate which are arranged in sequence. The second dielectric substrate is provided with an arched microstrip double-patch array, and the third dielectric substrate is provided with a conformal parasitic patch array; and aerogel is arranged between the first metal frame and the second dielectric substrate, between the second metal frame and the third dielectric substrate, and between the third</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN117410705A
source esp@cenet
subjects ANTENNAS, i.e. RADIO AERIALS
BASIC ELECTRIC ELEMENTS
ELECTRICITY
title Self-sensing surface radar structure for hypersonic flight environment
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-09T23%3A38%3A34IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=WANG%20WEI&rft.date=2024-01-16&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN117410705A%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true